- Owner type
- Co-owned, fractional ownership
- Serial number
- 6148
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 20, 2019
- Certificate issued
- July 3, 2025
- Expires
- July 31, 2032
- Mode S code
- A23525
Bombardier CL-600-2B16(CL-604)TCDS A21EAAirframe · Bombardier CL-600-2B16(CL-604)TCDS E15NEEngine · GE CF34-3B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 129
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1981 | 1 |
|---|---|
| 1982 | 6 |
| 1984 | 1 |
| 1988 | 1 |
| 1990 | 1 |
| 1991 | 2 |
| 1992 | 2 |
| 1993 | 1 |
| 1994 | 5 |
| 1995 | 5 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 3 |
| 2000 | 5 |
| 2001 | 7 |
| 2002 | 2 |
| 2003 | 4 |
| 2004 | 2 |
| 2005 | 5 |
| 2006 | 6 |
| 2007 | 6 |
| 2008 | 2 |
| 2009 | 5 |
| 2010 | 9 |
| 2011 | 3 |
| 2012 | 4 |
| 2013 | 3 |
| 2014 | 7 |
| 2015 | 4 |
| 2016 | 5 |
| 2017 | 8 |
| 2018 | 4 |
| 2019 | 5 |
| 2020 | 2 |
| 2021 | 4 |
| 2022 | 7 |
| 2023 | 8 |
| 2024 | 6 |
| 2025 | 3 |
| 2026 | 4 |
Airframe · Bombardier CL-600-2B16(CL-604)
AD 2026-14-09Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2026-07-01Landing gearInformation bulletins that may apply · 5
Advisory, not mandatory.
Airframe · Bombardier CL-600-2B16(CL-604)
SAIB AIR-21-15R1Navigation SystemSAIB NM-11-51Ice and Rain Protection: Wing Anti-Ice SystemSAIB NM-10-13Navigation: Flight Management SystemSAIB NE-03-28Engine · GE CF34-3B
SAIB NE-04-77Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N241QSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bombardier CL-600-2B16(CL-604) aircraft
FAA incident reports
No FAA accident or incident reports matched to N241QSMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Bombardier CL-600-2B16(CL-604) aircraft
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026051908121Coffeemaker · faultyFA NOTICED WISPY SMOKE FROM COFFEE MAKER. FO GOT UP TO LOOK AND SMOKE WAS ALREADY GONE, WITH NO SMELL NOTICED. IT LASTED MAYBE 20-30 SECONDS. COFFEE MAKER WAS TURNED OFF AND FLIGHT CONTINUED UNEVENTFULLY. CORRECTIVE ACTION: REMOVED FAULTY GALLEY COFFEE MAKER PSDR DXTA2025090204760Switch · faultedAFTER TAKEOFF OUT OF KTEB FLAP WAS RETRACTED WHEN WE WERE LEVEL AT 1500 FT MSL AND THE SPEED WAS 180KTS. FLAP HANDLE WAS AT ZERO, BUT FLAP INDICATION WAS AT 20, AND HAD THE FLAP FAIL MSG ON EICAS. RAN THE FLAP FAIL APPROACH QRC , DECLARED EMERGENCY WITHOUT SDR DXTA2025081904627Control Unit · malfunctionedUPON DEPARTURE FROM FFZ FLAPS WERE SET TO 0. FLAPS FAIL AMBER CAS ILLUMINATED FLAPS STILL SHOWED 20. FOLLOWED CHECKLIST SEND QRC FLAPS WOULD STILL NOT RETRACT ON GROUND. REMOVED FLAP CONTROL UNIT. INSTALLED FLAP CONTROL UNIT IAW AMM 27-51-04 OPERATIONAL TESTSDR DXTA2025071004171Support · out of adjustWHEN THE MAIN CABIN DOOR IS CLOSED THE SUPPORT LEG THAT THE DOOR RESTS ON WHEN OPEN IS NOT FULLY RECESSED WHEN THE DOOR IS CLOSED. IT¿S STICKING OUT APPROX THE WIDTH OF THE FOOT PLATE. CORRECTIVE ACTION; ADJUSTED MAIN DOOR SUPPORT LEG AS REQUIRED IAW AMM 52SDR DXTA2024062612175Pulley · defectiveMAIN DOOR MANUAL PULL HANDLE APPEARS TO BE OUT OF POSITION. MAIN DOOR CANNOT BE FULLY CLOSED OR FULLY OPEN. ( MANUAL HANDLE INTERFERES WITH BOTH THE CABLE AND PULLY ON THE LEFT AS VIEWED FROM INSIDE THE AIRCRAFT. INSPECTED MAIN DOOR, UNABLE TO OPEN DOOR DUESDR 3J7R2023032400001Bulb · burned outTECHS NOTED THE RH AFT OUTSIDE EMER LIGHT TO BE INOP.SDR DXTA2021120653020Lamp · brokenTHE AFT EXTERIOR EMERGENCY LIGHT IS INOP. // SIGNOFF // REMOVED AND REPLACED AFT EXTERIOR EMERGENCY LIGHT, ·IN REFERENCE TO CL 650 AMM 33-51-04 OPS CHECKS GOODSDR DXTA2021110151200Coalescer Bag · odorCABIN ODOR: OILY-SOCK SMELL OBSERVED DURING DESCENT IN GALLEY/CABIN. REPLACED LH & RH COALESCER SOCKS IAW CL-650 AMM 21-51-13. NO DEFECTS NOTED AT THIS TIME.
STCs that may be installed · 857
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Bombardier CL-600-2B16(CL-604)
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.